The MP was flying as lead of a two-ship formation during a dissimilar basic fighter maneuver
(BFM) sortie with an F-22A, assigned to the 525th Fighter Squadron. While maneuvering
defensively in relationship to the Mishap Wingman (MW), at approximately 5,400 feet mean sea
level (MSL) and 180 knots indicated airspeed (KIAS), the MP initiated a vertical climb to
65 degrees nose high, 20 degrees of right bank, 39 degrees Angle-of-Attack (AOA), and 1.2 Gs,
which apexed near 6,300 feet MSL and 105 KIAS, before a significant nose drop occurred. The
MP perceived the MA was not tracking as desired and initiated an unload of approximately one
fist-width’s forward stick with full right rudder. The nose pitched down and to the right to
65 degrees nose low, 110 degrees of right bank, -26 degrees AOA and G forces decreasing from
1.2 to -0.3 Gs. With right rudder still commanded, the MA experienced a negative G departure
from controlled flight with a snap roll entry to the left that transitioned to an inverted, negative G
spin. The MP received no indications of hydraulic, electrical, fuel, engine, structural, or flight
control system malfunctions. The MP was unable to recover the MA and ejected at approximately
1,100 feet MSL.
The Accident Investigation Board (AIB) President found, by a preponderance of the evidence, the
cause of the mishap was the MP’s improper application of forward stick with full right rudder,